A release mechanism for releasably securing a releasable structure to a stationary structure, where the mechanism employs release balls that can re-secure the releasable structure to the stationary structure. The release mechanism includes a base portion having three rails extending radially outward from a center of the base portion, and a rotatable portion rotatably mounted to the base portion, where the rotatable portion has a cam indentation. The release balls are positioned between the base portion and the rotatable portion so that one of the release balls is ridable on each of the rails and all of the release balls are positioned within the cam indentation. The cam indentation is configured so that as the rotatable portion is rotated relative to the base portion the cam indentation causes and allows the release balls to move along the rails in unison with each other to hold and release the releasable structure.
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1. A release mechanism comprising:
a base portion including a plurality of equally spaced rails extending radially outward from a center of the base portion;
a rotatable portion rotatably mounted to the base portion, said rotatable portion including a bottom surface having a cam indentation; and
a plurality of release balls positioned between the base portion and the rotatable portion so that one of the release balls is ridable on each of the rails and all of the release balls are positioned within the cam indentation, said cam indentation being configured so that as the rotatable portion is rotated relative to the base portion the cam indentation causes the release balls to move along the rails to the center and allows the release balls to move outward away from the center in unison with each other.
9. A release mechanism for releasably securing a releasable structure to a stationary structure, said mechanism comprising:
a base portion including three equally spaced rails extending radially outward from a center of the base portion and an opening extending through the center of the base portion;
a rotatable portion rotatably mounted to the base portion and including an opening in axial alignment with the opening in the base portion, said releasable structure extending through the openings and said rotatable portion including a bottom surface having a cam indentation; and
three release balls positioned between the base portion and the rotatable portion so that one of the release balls is ridable on each of the rails and all of the release balls are positioned within the cam indentation, said cam indentation being configured so that as the rotatable portion is rotated relative to the base portion the cam indentation causes the release balls to move along the rails to the center and allows the release balls to move outward away from the center in unison with each other so that when the release balls are at an end of the rails proximate to the center of the base portion the mechanism holds the releasable structure and when the release balls are at an end of the rails opposite to the center of the base portion the mechanism releases the releasable structure.
15. A release joint assembly comprising:
a stationary structure including an opening;
a releasable structure;
a bolt secured to the releasable structure and extending through the opening in the stationary structure; and
a release mechanism for releasing the releasable structure from the stationary structure, said release mechanism including a base portion having a center opening and a plurality of equally spaced rails extending radially outward from the center opening of the base portion, a rotatable portion rotatably mounted to the base portion, said rotatable portion including a center opening in axial alignment with the center opening in the base portion and a bottom surface having a cam indentation, said bolt extending through the axially aligned center openings, and a plurality of release balls positioned between the base portion and the rotatable portion so that one of the release balls is ridable on each of the rails and all of the release balls are positioned within the cam indentation, said cam indentation being configured so that as the rotatable portion is rotated relative to the base portion the cam indentation causes the release balls to move along the rails to the center and allows the release balls to move outward away from the center in unison with each other in manner so that the release structure is secured to the stationary structure when the release balls are positioned proximate the center openings and the release structure is released from the stationary structure when the release balls are at an end of the rails opposite to the center openings.
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The Government of the United States of America has rights in this invention pursuant to a U.S. Government contract.
This disclosure relates generally to a reusable release mechanism and, more particularly, to a reusable release mechanism for releasably securing a releasable structure to a stationary structure, where the mechanism employs slidable release balls that can re-secure the releasable structure to the stationary structure.
Various applications, for example, spacecraft applications, require a releasable joint mechanism, such as a non-explosive actuator (NEA), where typically a bolt having a head is secured to a releasable structure and is releasably mounted to a stationary structure. In one known design, the bolt extends through a bore in the stationary structure, where the head of the bolt is prevented from passing through the bore by a three-piece split washer. A wire is wrapped around the washer to hold the pieces together, where the wire is under compression, and a fusible link holds the wire in compression. A current is applied to the link to melt it and release the wire, which causes the pieces of the washer to separate and allow the head of the bolt to pass through the bore under a certain force, such as a spring force or gravity, thus releasing the releasable structure from the stationary structure. However, in this and other similar designs, once the releasable structure is released, the joint is not reusable for re-securing the releasable structure to the stationary structure.
There may be various applications for joint mechanisms of the type discussed above where it is desirable to reuse the joint mechanism in a manner that allows the releasable structure to be re-secured to the stationary structure, for example, to save cost, the mechanism may not be accessible, and other benefits.
The following discussion of the embodiments of the disclosure directed to a reusable release mechanism for releasably securing a releasable structure to a stationary structure, where the mechanism employs slidable release balls that can re-secure the releasable structure to the stationary structure is merely exemplary in nature, and is in no way intended to limit the disclosure or its applications or uses.
If the rotatable portion 52 was continually rotated in one direction, the release balls 42 would be caused to move inward and allowed to move outward along the rails 70 as the rotatable portion 52 rotates. In order to limit the rotation of the rotatable portion 52 and provide a mechanism for locking the rotatable portion 52 in the latched and/or unlatched position, the release mechanism 40 includes a stop block 82 that is secured to the base portion 50 by a pull pin 84 inserted into an orifice 78 and the rotating portion 52 includes a tab 80. When the rotatable portion 52 rotates, the tab 80 will engage the stop block 82 and hold the rotatable portion 52 so that the release balls 42 are locked or held in the latched or unlatched position.
The foregoing discussion discloses and describes merely exemplary embodiments of the present disclosure. One skilled in the art will readily recognize from such discussion and from the accompanying drawings and claims that various changes, modifications and variations can be made therein without departing from the spirit and scope of the disclosure as defined in the following claims.
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Apr 20 2020 | Northrop Grumman Systems Corporation | (assignment on the face of the patent) | / | |||
Apr 20 2020 | SABO, SCOTT G | Northrop Grumman Systems Corporation | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 052441 | /0070 |
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